Acoustic environments of the F-111A aircraft during ground runup /
John N. Cole and Justus F. Rose.

Description

Main Author

Cole, John N.

Related Names

Rose, Justus F., author.
Aerospace Medical Research Laboratories (U.S.)

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Aerospace Medical Research Laboratories, Aerospace Medical Division, Air Force Systems Command, United States Air Force, 1968.

Subjects

Jet fighter planes.
F-111 (Jet fighter plane) > F-111 (Jet fighter plane) / Noise.
Jet fighter planes > Jet fighter planes / United States > Jet fighter planes / United States / Noise.
United States.

Summary

Sound pressure level measurements were made on an F-111A aircraft at 250-foot radial distance with three different engine power configurations at Wright-Patterson AFB, Ohio. In addition, sound level measurements were made at four maintenance positions where personnel would typically be located during normal ground operations. These data were used to compute the power spectra, directivity indices, equal sound pressure level contours, equal perceived noise level contours, and equal speech interference level contours. These results are presented in graphical form and can be used to determine the acoustic environments at distances from 125 to 6000 feet from the aircraft during ground operation. (Author).

Note

"May 1968."

Physical Description

vi, 50 pages : illustrations ; 28 cm.

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